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RESEARCH PAPERS

Discharge Coefficient Measurements of Film-Cooling Holes With Expanded Exits

[+] Author and Article Information
M. Gritsch, A. Schulz, S. Wittig

Lehrstuhl und Institut für Thermische Strömungsmaschinen, Universität Karlsruhe (T.H.), Kaiserstr, 12, 76128 Karlsruhe, Germany

J. Turbomach 120(3), 557-563 (Jul 01, 1998) (7 pages) doi:10.1115/1.2841753 History: Received February 01, 1997; Online January 29, 2008

Abstract

This paper presents the discharge coefficients of three film-cooling hole geometries tested over a wide range of flow conditions. The hole geometries include a cylindrical hole and two holes with a diffuser-shaped exit portion (i.e., a fan-shaped and a laidback fan-shaped hole). The flow conditions considered were the crossflow Mach number at the hole entrance side (up to 0.6), the crossflow Mach number at the hole exit side (up to 1.2), and the pressure ratio across the hole (up to 2). The results show that the discharge coefficient for all geometries tested strongly depends on the flow conditions (crossflows at hole inlet and exit, and pressure ratio). The discharge coefficient of both expanded holes was found to be higher than of the cylindrical hole, particularly at low pressure ratios and with a hole entrance side crossflow applied. The effect of the additional layback on the discharge coefficient is negligible.

Copyright © 1998 by The American Society of Mechanical Engineers
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